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유춘상

Yoo, Chun Sang
Combustion and Propulsion Lab.
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dc.citation.endPage 1921 -
dc.citation.number 2 -
dc.citation.startPage 1913 -
dc.citation.title PROCEEDINGS OF THE COMBUSTION INSTITUTE -
dc.citation.volume 38 -
dc.contributor.author Van, Kyu Ho -
dc.contributor.author Oh, Suhyeon -
dc.contributor.author Cha, Min Suk -
dc.contributor.author Yoo, Chun Sang -
dc.contributor.author Pakr, Jeong -
dc.contributor.author Chung, Suk Ho -
dc.date.accessioned 2023-12-21T16:08:31Z -
dc.date.available 2023-12-21T16:08:31Z -
dc.date.created 2020-09-08 -
dc.date.issued 2021-04 -
dc.description.abstract Stabilization characteristics of laminar lifted jet flames in a coflow were investigated experimentally to elucidate the effect of Schmidt number in methane and ethylene fuels diluted with N 2 , He, and Ar. A nonmonotonic (decreasing and then increasing) liftoff height ( H L ) behavior with jet velocity ( U 0 ) was observed previously for methane fuel diluted with N 2 . To further elucidate the fuel Schmidt number (Sc F ) effect in exhibiting such a non-monotonic (U-shaped) behavior, various diluents (N 2 , He, and Ar) were added to the fuel streams and methane and/or ethylene fuels were used. The result showed three flame types in terms of Sc F and fuel density; nozzle-attached flame, stationary lifted flame, and oscillating flame. Among stationary lifted flames, two distinct H L behaviors with U 0 were observed; monotonic and non-monotonic H L behaviors. A critical Schmidt number (Sc F,cr1 ) existed over which monotonically increasing behavior was observed. A second critical Schmidt number (Sc F,cr2 ) also existed such that U-shaped behavior was observed for Sc F,cr2 < Sc F < Sc F,cr1 . An oscillating lifted flame was observed for Sc F < Sc F,cr2 . The oscillating and stationary lifted flames can be categorized in terms of the density differences among the fuel, air, and burnt gas. For the increasing H L cases (including the increasing regime in U-shaped behavior), H L behavior can be characterized in terms of Sc F , the density difference between fuel and air, Sc F,cr1 , and U 0 . While the decreasing H L regime in the U-shaped behavior can be characterized with Sc F and/or the Richardson number (defined based on the density difference between fuel and air). Oscillating flames were observed with the frequency range of 2.1 & ndash;2.7 Hz by the repetitive action of positive (by burnt gas) and negative (when the fuel heavier than air) buoyancies. -
dc.identifier.bibliographicCitation PROCEEDINGS OF THE COMBUSTION INSTITUTE, v.38, no.2, pp.1913 - 1921 -
dc.identifier.doi 10.1016/j.proci.2020.06.344 -
dc.identifier.issn 1540-7489 -
dc.identifier.scopusid 2-s2.0-85090999778 -
dc.identifier.uri https://scholarworks.unist.ac.kr/handle/201301/48049 -
dc.identifier.url https://www.sciencedirect.com/science/article/pii/S1540748920304375?via%3Dihub -
dc.identifier.wosid 000651831800002 -
dc.language 영어 -
dc.publisher ELSEVIER SCIENCE INC -
dc.title Effects of Schmidt number on non-monotonic liftoff height behavior in laminar coflow-jet flames with diluted methane and ethylene -
dc.type Article -
dc.description.isOpenAccess FALSE -
dc.relation.journalWebOfScienceCategory Thermodynamics; Energy & Fuels; Engineering, Chemical; Engineering, Mechanical -
dc.relation.journalResearchArea Thermodynamics; Energy & Fuels; Engineering -
dc.type.docType Article -
dc.description.journalRegisteredClass scie -
dc.description.journalRegisteredClass scopus -
dc.subject.keywordAuthor Lifted flame -
dc.subject.keywordAuthor Coflow jet -
dc.subject.keywordAuthor Schmidt number -
dc.subject.keywordAuthor Buoyancy -
dc.subject.keywordAuthor Edge flame -
dc.subject.keywordPlus OSCILLATING LIFTED FLAMES -
dc.subject.keywordPlus TRIBRACHIAL FLAMES -
dc.subject.keywordPlus SELF-EXCITATION -
dc.subject.keywordPlus STABILIZATION -
dc.subject.keywordPlus PROPAGATION -
dc.subject.keywordPlus EDGE -

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